ICBM Mark 2 vehicle employed spherical capsule to gather data on flight trajectories, which was ejected from nose cone afterbody to be recovered by ships; in design of capsule problem of secondary body ejection through trailing wake of prime body was examined; integrated wake/capsule interaction phenomena that occur during separation of 2 bodies.
Data capsule ejection through re-entry body wake
Aerospace Eng
Aerospace Engineering ; 20 , n 5
1961
2 pages
Article (Journal)
English
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Space capsule ejection assembly Patent
NTRS | 1966
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